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GB2524438A - Electric power connector for aircraft drive wheel drive system - Google Patents

Electric power connector for aircraft drive wheel drive system Download PDF

Info

Publication number
GB2524438A
GB2524438A GB1513053.7A GB201513053A GB2524438A GB 2524438 A GB2524438 A GB 2524438A GB 201513053 A GB201513053 A GB 201513053A GB 2524438 A GB2524438 A GB 2524438A
Authority
GB
United Kingdom
Prior art keywords
aircraft
electric
electric power
drive means
drive wheel
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB1513053.7A
Other versions
GB201513053D0 (en
GB2524438B (en
Inventor
Jonathan Sidney Edelson
Arlie Stonestreet
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Borealis Technical Ltd
Original Assignee
Borealis Technical Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Borealis Technical Ltd filed Critical Borealis Technical Ltd
Publication of GB201513053D0 publication Critical patent/GB201513053D0/en
Publication of GB2524438A publication Critical patent/GB2524438A/en
Application granted granted Critical
Publication of GB2524438B publication Critical patent/GB2524438B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/405Powered wheels, e.g. for taxing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/34Alighting gear characterised by elements which contact the ground or similar surface  wheeled type, e.g. multi-wheeled bogies
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R12/00Structural associations of a plurality of mutually-insulated electrical connecting elements, specially adapted for printed circuits, e.g. printed circuit boards [PCB], flat or ribbon cables, or like generally planar structures, e.g. terminal strips, terminal blocks; Coupling devices specially adapted for printed circuits, flat or ribbon cables, or like generally planar structures; Terminals specially adapted for contact with, or insertion into, printed circuits, flat or ribbon cables, or like generally planar structures
    • H01R12/70Coupling devices
    • H01R12/7076Coupling devices for connection between PCB and component, e.g. display
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K13/00Structural associations of current collectors with motors or generators, e.g. brush mounting plates or connections to windings; Disposition of current collectors in motors or generators; Arrangements for improving commutation
    • H02K13/02Connections between slip-rings and windings
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K13/00Structural associations of current collectors with motors or generators, e.g. brush mounting plates or connections to windings; Disposition of current collectors in motors or generators; Arrangements for improving commutation
    • H02K13/04Connections between commutator segments and windings
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K3/00Details of windings
    • H02K3/46Fastening of windings on the stator or rotor structure
    • H02K3/50Fastening of winding heads, equalising connectors, or connections thereto
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K5/00Casings; Enclosures; Supports
    • H02K5/04Casings or enclosures characterised by the shape, form or construction thereof
    • H02K5/22Auxiliary parts of casings not covered by groups H02K5/06-H02K5/20, e.g. shaped to form connection boxes or terminal boxes
    • H02K5/225Terminal boxes or connection arrangements
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/14Structural association with mechanical loads, e.g. with hand-held machine tools or fans
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K1/00Printed circuits
    • H05K1/02Details
    • H05K1/0213Electrical arrangements not otherwise provided for
    • H05K1/0263High current adaptations, e.g. printed high current conductors or using auxiliary non-printed means; Fine and coarse circuit patterns on one circuit board
    • H05K1/0265High current adaptations, e.g. printed high current conductors or using auxiliary non-printed means; Fine and coarse circuit patterns on one circuit board characterized by the lay-out of or details of the printed conductors, e.g. reinforced conductors, redundant conductors, conductors having different cross-sections
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K2201/00Indexing scheme relating to printed circuits covered by H05K1/00
    • H05K2201/09Shape and layout
    • H05K2201/09209Shape and layout details of conductors
    • H05K2201/09218Conductive traces
    • H05K2201/09227Layout details of a plurality of traces, e.g. escape layout for Ball Grid Array [BGA] mounting
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/80Energy efficient operational measures, e.g. ground operations or mission management

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Motor Or Generator Frames (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

An electric connector assembly is provided that is designed to provide a simple and reliable electric connection between a source of electric power on an aircraft and a plurality of electrical connections, such as those from stator windings, in an electric drive means powering an aircraft landing gear drive wheel. The plurality of drive means electrical connections are individually connected to power distribution elements designed to significantly reduce the number of connectors required to establish an electrical connection between the drive means and an aircraft power supply. The reduced number of connectors is directed out of the wheel and guided along a path by a path guide element to a connector element designed to connect directly with a wire harness or other connection with an aircraft source of electric power. This electric connector design facilitates disconnection and reconnection when removal and remounting of the drive wheel is required.
GB1513053.7A 2012-12-24 2013-12-24 Electric power connector for aircraft drive wheel drive system Active GB2524438B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201261745762P 2012-12-24 2012-12-24
PCT/US2013/077678 WO2014105894A2 (en) 2012-12-24 2013-12-24 Electric power connector for aircraft drive wheel drive system

Publications (3)

Publication Number Publication Date
GB201513053D0 GB201513053D0 (en) 2015-09-09
GB2524438A true GB2524438A (en) 2015-09-23
GB2524438B GB2524438B (en) 2019-06-12

Family

ID=51022195

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1513053.7A Active GB2524438B (en) 2012-12-24 2013-12-24 Electric power connector for aircraft drive wheel drive system

Country Status (3)

Country Link
US (1) US9725163B2 (en)
GB (1) GB2524438B (en)
WO (1) WO2014105894A2 (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2874786C (en) 2012-05-25 2022-02-01 Genesis Advanced Technology Inc. Speed change device
CA2968616C (en) 2014-01-30 2022-08-23 Genesis Advanced Technology Inc. Roller drive
FR3024706B1 (en) * 2014-08-05 2018-03-23 Messier Bugatti Dowty TRANSMISSION OF TORQUE TO THE WHEEL BY THE RIM ASSEMBLING BOLTS
GB2534541B (en) * 2014-11-30 2020-11-04 Borealis Tech Ltd Method for increasing aircraft effective value
KR102359816B1 (en) 2017-09-16 2022-02-08 제네시스 어드밴스드 테크놀러지 인크. differential planetary gearbox
US11211184B2 (en) 2019-01-23 2021-12-28 Pratt & Whitney Canada Corp. System of harness and engine case for aircraft engine
FR3108559B1 (en) * 2020-03-27 2024-03-15 Safran Landing Systems Aircraft wheel with drive pins
US11852024B2 (en) 2020-12-18 2023-12-26 Ge Aviation Systems Llc Electrical strut for a turbine engine

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020027395A1 (en) * 2000-06-09 2002-03-07 Ricoh Company, Ltd. DC motor
US20030048084A1 (en) * 1998-01-23 2003-03-13 Brown Fred A. Low profile motor
US20100320853A1 (en) * 2009-06-18 2010-12-23 Aisin Seiki Kabushiki Kaisha Electric motor having wire connection structure and wire connection method for the same
US20100326748A1 (en) * 2006-12-15 2010-12-30 Oto Melara S.P.A. Con Unico Socio Power-driven wheel for a military vehicle
US20120098366A1 (en) * 2009-06-24 2012-04-26 Masashi Yamasaki Drive apparatus
US20120168557A1 (en) * 2010-11-02 2012-07-05 Borealis Technical Limited Integrated Aircraft Ground Navigation Control System

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6838791B2 (en) 2000-11-15 2005-01-04 Borealis Technical Limited Mesh connected electrical rotating machine with span changing
US6657334B1 (en) 2000-10-23 2003-12-02 Borealis Technical Limited High phase order motor with mesh connected windings
JP3248830B2 (en) 1995-06-30 2002-01-21 本田技研工業株式会社 Electric wheel motor
DE19902837C1 (en) 1999-01-20 2000-08-10 Siemens Ag Rotating electrical machine with permanently excited rotor
US20030176085A1 (en) 2002-02-25 2003-09-18 Atl Technology, Lc. Electrical connector assembly
US7469858B2 (en) 2003-10-09 2008-12-30 Borealis Technical Limited Geared wheel motor design
US20060273686A1 (en) 2004-06-21 2006-12-07 Edelson Jonathan S Hub motors

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030048084A1 (en) * 1998-01-23 2003-03-13 Brown Fred A. Low profile motor
US20020027395A1 (en) * 2000-06-09 2002-03-07 Ricoh Company, Ltd. DC motor
US20100326748A1 (en) * 2006-12-15 2010-12-30 Oto Melara S.P.A. Con Unico Socio Power-driven wheel for a military vehicle
US20100320853A1 (en) * 2009-06-18 2010-12-23 Aisin Seiki Kabushiki Kaisha Electric motor having wire connection structure and wire connection method for the same
US20120098366A1 (en) * 2009-06-24 2012-04-26 Masashi Yamasaki Drive apparatus
US20120168557A1 (en) * 2010-11-02 2012-07-05 Borealis Technical Limited Integrated Aircraft Ground Navigation Control System

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
JONES, David. PCB Design Tutorial. [online], June 2004 [retrieved on 2015-03-30]. Retrieved from the Internet: *

Also Published As

Publication number Publication date
US9725163B2 (en) 2017-08-08
GB201513053D0 (en) 2015-09-09
GB2524438B (en) 2019-06-12
WO2014105894A3 (en) 2015-07-16
WO2014105894A2 (en) 2014-07-03
US20150336660A1 (en) 2015-11-26

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Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)

Free format text: REGISTERED BETWEEN 20241107 AND 20241113